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MMPDS-01<br />

31 January 2003<br />

Figure 2.3.1.5.9. Fatigue-crack-propagation data for 0.80-inch D6AC<br />

<strong>steel</strong> alloy plate. Data include material both oil quenched and salt<br />

quenched (TUS: 230-240 ksi). [Reference - 2.3.1.5.9.]<br />

Specimen Thickness: 0.70-0.75 inch Environment: Dry air and lab air<br />

Specimen Width: 1.5-5.0 inches Temperature: RT<br />

Specimen Type: CT Orientation: L-T<br />

2-65

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